TASK 53-05-03-210-820
23. INTERNAL - GENERAL VISUAL: AREA ABOVE MAIN LANDING GEAR WHEEL WELL
(Figure 225)
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
137 Area Above M.L.G. Wheel Well, Body Station 663.75 to Body Station 727 - Left
138 Area Above M.L.G. Wheel Well, Body Station 663.75 Body Station 727 - Right
B. Access Panels
Number Name/Location
S1302 Area Above Main Landing Gear Wheel Well Inspection
C. Inspection
SUBTASK 53-05-03-010-018
(1) Open this access panel:
Number Name/Location
S1302 Area Above Main Landing Gear Wheel Well Inspection
NOTE: Remove floor panels. Remove/displace insulation blankets as required.
SUBTASK 53-05-03-210-020
(2) Do a General Visual inspection of the fuselage lower lobe above main landing gear wheel well,
including:
1. Pressure deck web to stiffeners, stiffener attachment to floor beam at STA 727.
2. Side skin panels, circumferential skin and stringer splice.
3. Bulkheads at STA 663 and 727.
4. Side strut support frame at STA 706.
5. Main landing gear support frame at STA 695 and 716.
6. Wheel well frame at STA 685.
SUBTASK 53-05-03-910-023
(3) 737-6789 Basic Task Description, AMM Task 51-05-01-210-808.
SUBTASK 53-05-03-410-018
(4) Close this access panel:
Number Name/Location
S1302 Area Above Main Landing Gear Wheel Well Inspection
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-03
Page 278
D633A101-ILF Jun 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
To Next Page
Loading...
